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一种用于获取SiC/SiC复合材料力学参数的新型反分析方法及其在涡轮盘损伤评估中的应用

A Novel Inverse Analysis Method for Mechanical Parameter Acquisition in SiC/SiC Composites and Its Application to Turbine Disc Damage Assessment.

作者信息

Wang Wenjun, Zeng Qi, Li Chaochao, Li Min, Cao Liang, Chen Guoqing, Cao Peng

机构信息

AECC Hunan Aviation Powerplant Research Institute, Zhuzhou 412002, China.

School of Aerospace Engineering, Xiamen University, Xiamen 361102, China.

出版信息

Materials (Basel). 2025 Jan 2;18(1):160. doi: 10.3390/ma18010160.

Abstract

Obtaining the mechanical parameters of SiC/SiC composites quickly and accurately is crucial for the performance evaluation and optimal design of novel turbine disc structures. A representative volume element (RVE) model of 2D woven SiC/SiC composites was developed using CT scanning and machine learning-driven image reconstruction techniques. The stress-strain curve was obtained by uniaxial tensile test, and the anisotropic mechanical parameters were obtained by inverse analysis using a non-dominated sorting genetic algorithm (NSGA-II). Subsequently, the uniaxial tension simulation was carried out based on the RVE model and mechanical parameters. The results show that the simulation curve is in good agreement with the test, and the errors of initial modulus and peak stress were 3.98% and 2.75%, respectively. Finally, the finite element models of the turbine disc with two braiding schemes were established to simulate the damage of the turbine disc. And the simulation results were verified by a centrifugal test. The failure modes of the two kinds of turbine discs are similar to the centrifugal test results, and the maximum rotating speed was close to the test results. The findings of this study provide a novel solution for obtaining the anisotropic mechanical parameters of SiC/SiC composites with different woven schemes.

摘要

快速准确地获取SiC/SiC复合材料的力学参数对于新型涡轮盘结构的性能评估和优化设计至关重要。利用CT扫描和机器学习驱动的图像重建技术建立了二维编织SiC/SiC复合材料的代表性体积单元(RVE)模型。通过单轴拉伸试验获得应力-应变曲线,并使用非支配排序遗传算法(NSGA-II)通过反分析获得各向异性力学参数。随后,基于RVE模型和力学参数进行了单轴拉伸模拟。结果表明,模拟曲线与试验结果吻合良好,初始模量和峰值应力的误差分别为3.98%和2.75%。最后,建立了两种编织方案的涡轮盘有限元模型,模拟涡轮盘的损伤情况。并通过离心试验对模拟结果进行了验证。两种涡轮盘的失效模式与离心试验结果相似,最大转速接近试验结果。本研究结果为获取不同编织方案的SiC/SiC复合材料各向异性力学参数提供了一种新的解决方案。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/7713/11722191/22a1cd60e670/materials-18-00160-g001.jpg

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